N286AS
Registered owner: ATLANTIC AVIATION INTERNATIONAL INC, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
18 reports on file, 1998-11-16 – 2002-05-25.
Part: BRACKET — CRACKED (LT MLG DOOR)
DURING HANGER MAINTENANCE, THE LEFT MAIN LANDING GEAR FORWARD OUTBOARD DOOR AFT TENSIONER BRACKET HAD A CRACK. THE LEFT MAIN LANDING GEAR FORWARD INBOARD DOOR AFT HINGE ANGLE WAS ALSO DISCOVERED WITH A CRACK. MAINTENANCE REMOVED AND REPLACED BOTH THE CRACKED TENSIONER BRACKET AND THE CRACKED HINGE ANGLE. AIRCRAFT RETURNED TO SERVICE.
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT HAD CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)
Part: SILL — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL PLATE BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-04, AND 51-40-02. (M)
Part: CROSSBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT OUTBOARD CROSSBEAM AT FRAME 16. CORROSION WAS ALSO FOUND ON THE LEFT INBOARD CROSS BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM'S 51-40-05, 51-40-02, AND 51-25-00. (M)
Part: BUTT STRAP — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 15 AND 21 AND ALSO FROM FRAME 21 TO FRAME 25. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF BUTT STRAP IAW SRM 51-25-00, 51-21-00, AND 51-40-02. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPCTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-02, 51-25-00, AND 51-21-02. (M)
Part: CROSSBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS CORRODED AT FRAME 20. CORROSION WAS ALSO FOUND ON THE LEFT OUTBOARD CROSS BEAM (P/N 120-14243-001) AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRMS 51-21-04, 51-21-05, 51-25-00, AND 51-40-02. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)
Part: CROSSBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD CROSSBEAM HAD CORROSION AT FRAME 16. THE RIGHT OUTBOARD CROSSBEAM ALSO HAD CORROSION AT FRAME 18. MAINTENANCE REMOVED AND REPLACED CORRODED CROSSBEAMS IAW SRM 51-40-02. (M)
Part: BUTT STRAP — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRMS 51-40-02, 51-25-00, 51-21-02 AND 51-21-00. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 17 LEFT BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRIGNER IAW SRM 51-40-00. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15A. CORROSION WAS ALSO FOUND ON THE SAME STRINGER BETWEEN FRAMES 16 AND 18A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-00, 51-25-00, AND 51-21-00. (M)
Earlier reports · 1998–2001 · 6 reports
2001
Part: ODOR — DETECTED (COCKPIT)
UPON DEPARTURE FROM OKC, AT APPROXIMATELY 5000 FEET, CAPTAIN STARTED TO SMELL A HOT BURNING ODOR COMING FROM THE AIR VENTS. HE TURNED THE PACKS OFF, AND THE SMELL WENT AWAY. NO WARNING INDICATIONS WERE RECEIVED FROM THE AIR CONDITIONING SYSTEM. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AND OPERATED PACKS BUT COULD NOT DUPLICATE THE SMELL. ENGINE AND PACKS BOTH OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M)
2000
Part: SKIN — CRACKED (FUSELAGE)
FUSELAGE SKIN BULGES WITH .50 INCH CRACK IN OUTER SKIN AT FR 23 BS 7654.7 BETWEEN STR 20L AND STR 21L. ALSO, A .50 INCH CRACK BETWEEN STR 21L AND STR 21R, BS 7654.7. THIS CORROSION IS A RESULT OF THE DIRECT CONTACT BETWEEN THE FUSELAGE SKIN PANEL AND THE TITANIUM STRAP AT THIS FRAME. C/W EMB120 SB 120-53-0065 AFTER APPLICABLE REPAIRS ARE COMPLETED. (X)
1999
Part: SEAL — DETACHED (CARGO DOOR)
FLT 4067 - EN ROUTE ATL-CRW, LOST PRESSURIZATION AT 25,000 FEET AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. OXYGEN MASKS WERE DEPLOYED IN THE CABIN. LANDING WAS MADE SAFELY AT CRW WITHOUT FURTHER INCIDENT. LOCAL MTC FOUND CARGO DOOR SEAL DETACHED FROM LOWER FORWARD CORNER OF DOOR AND RESECURED SEAL, ALSO RESTOWED THE OXYGEN MASKS. FOLLOWUP INSPECTION BY ATL MTC DETERMINED THAT THE FORWARD LOWER SECTION OF THE CARGO DOOR SEAL RETAINER WAS FAULTY AND REPLACED THE RETAINER. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)
1998
Part: FRAME — CRACKED (LT NACELLE)
FLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISPREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE REMAINS UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS AND SUGGEST TIMED INTERVALS FOR REPETITIVE INSPECTION OF AREA.
Part: FRAME — CRACKED (RT NACELLE)
FLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS AND WOULD SUGGEST TIMED INTERVALS AND REPETITIVE INSPECTION OF AREA.
Part: FRAME — CRACKED (LT/RT NACELLE)
DURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)